A reflective paint's liquid mixture includes 42.4-71.3 weight percent of a liquid solvent, 14.4-28.3 weight percent of a binder fully dissolved in the liquid solvent, and 13.8-29.3 weight percent of light scattering particles that are insoluble in the liquid solvent and are of a size ranging from 100 nanometers to 200 nanometers. The binder is selected from potassium bromide, sodium chloride, potassium chloride, sodium bromide, cesium chloride, and rubidium chloride. The light scattering particles are selected from hafnium oxide and yttrium oxide. The reflective paint is particularly useful as a surface coating for a variety of structures that must support cryogenic temperatures. It can be used in any application to act as a broadband reflector of the Sun's radiation in the wavelength band from approximately 0.21 microns to 9 microns and beyond.
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20. A reflective paint, comprising a liquid mixture that includes:
42.4-71.3 weight percent purified water,
14.4-28.3 weight percent of potassium bromide having a material purity of at least 99.9 percent, and
13.8-29.3 weight percent of yttrium oxide particles having a material purity of at least 99.9 percent, said yttrium oxide particles having a size ranging from 100 nanometers to 200 nanometers.
1. A reflective paint, comprising a liquid mixture that includes:
42.4-71.3 weight percent of a liquid solvent,
14.4-28.3 weight percent of a binder fully dissolved in said liquid solvent, said binder being selected from the group of materials consisting of potassium bromide, sodium chloride, potassium chloride, sodium bromide, cesium chloride, and rubidium chloride, and
13.8-29.3 weight percent of light scattering particles that are insoluble in said liquid solvent and are of a size ranging from 100 nanometers to 200 nanometers, said light scattering particles selected from the group of materials consisting of hafnium oxide and yttrium oxide.
12. A reflective paint, comprising a liquid mixture that includes:
42.4-71.3 weight percent purified water,
14.4-28.3 weight percent of a binder having a material purity of at least 99.9 percent, said binder comprising a single material selected from the group consisting of potassium bromide, sodium chloride, potassium chloride, sodium bromide, cesium chloride, and rubidium chloride, and
13.8-29.3 weight percent of light scattering particles having a material purity of at least 99.9 percent, said light scattering particles having a size ranging from 100 nanometers to 200 nanometers, said light scattering particles comprising a single material selected from the group consisting of hafnium oxide and yttrium oxide.
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Pursuant to 35 U.S.C. § 119, this patent application claims the benefit of priority to U.S. Provisional Patent Application Ser. No. 62/740,597, filed Oct. 3, 2018, the contents of which are hereby incorporated by reference in their entirety.
The invention described herein was made in the performance of work under a NASA contract and by employees of the United States Government and is subject to the provisions of Public Law 96-517 (35 U.S.C. § 202), and may be manufactured and used by or for the Government for governmental purposes without the payment of any royalties thereon or therefore.
This invention relates to reflective coatings. More specifically, the invention is a reflective paint that can be applied to surfaces for the preservation of cryogenic temperatures for objects in space to thereby reduce or eliminate the need for active cooling.
There are many temperature-related challenges involved in deep-space exploration, but several of these can be mitigated, or even solved, by the development of a coating that reflects most of the Sun's energy, yet still provides far-infrared heat emission. Such a coating would allow non-heat-generating objects in space to reach cryogenic temperatures without using an active cooling system. This would benefit deep-space sensors that require low temperatures, such as the James Webb Telescope focal plane array. It would also allow the use of superconductors in deep space, which could enable technologies such as magnetic energy storage rings; lossless power delivery; or large-volume magnetic shields for protection of space structures against galactic cosmic radiation. However, perhaps the most significant enablement achieved from such a coating would be the long-term, deep space storage of cryogenic liquids, such as liquid oxygen (LOX).
Selective surfaces, also known as thermal control coatings, are often used in spacecraft applications to minimize the absorption of solar radiation, yet allow infrared (IR) energy to be emitted. These coatings allow the emission of waste heat while minimizing the solar heat load thereby providing thermal control of spacecraft. The best currently-available solar reflectors absorb 6% of the Sun's power in the 250 nanometer (nm) to 2500 nm range and absorb additional solar power at wavelengths longer than 2500 nm. Therefore, state-of-the-art solar reflectors likely absorb more than 100 watts per meter squared (W/m2) of the Sun's irradiant power, while emitting roughly 400 W/m2 when at 300° Kelvin (K). This allows a net energy loss providing cooling to a spacecraft. However, if a plate were covered with this solar reflector and turned to face the Sun, it would come to an equilibrium temperature of about 200° K assuming no heat flowed out of the back of the plate. While 200° K is a cold temperature, it is not cold enough to allow storage of cryogens or to permit operation of superconductors.
Accordingly, it is an object of the present invention to provide a reflective coating/surface for cryogenic applications.
Another object of the present invention is to provide a reflective paint that can readily be applied to a variety of structures.
Other objects and advantages of the present invention will become more obvious hereinafter in the specification and drawings.
In accordance with the present invention, a reflective paint is a liquid mixture that includes
42.4-71.3 weight percent of a liquid solvent,
14.4-28.3 weight percent of a binder fully dissolved in the liquid solvent, and
13.8-29.3 weight percent of light scattering particles that are insoluble in the liquid solvent and are of a size ranging from 100 nanometers to 200 nanometers.
The binder is selected from the group of materials consisting of potassium bromide, sodium chloride, potassium chloride, sodium bromide, cesium chloride, and rubidium chloride. The light scattering particles are selected from the group of materials consisting of hafnium oxide and yttrium oxide.
Other objects, features, and advantages of the present invention will become apparent upon reference to the following description of the preferred embodiments and to the drawings, wherein corresponding reference characters indicate corresponding parts throughout the several views of the drawings and wherein:
The present invention is a reflective paint that is particularly useful as a surface coating for a variety of structures that must support cryogenic temperatures. For example, the reflective paint of the present invention can be used on a variety of structures and systems used in space that are dependent upon maintenance of very cold (i.e., cryogenic) temperatures for system operation and/or the structure's contents. Further, the reflective paint of the present invention could be used to reduce or eliminate the need to employ active cooling systems onboard space systems and structures. However, it is to be understood that the reflective paint of the present invention is not limited to in-space applications as the reflective paint can be used in any application to act as a broadband reflector of the Sun's radiation in the wavelength band from approximately 0.21 microns to 9 microns and beyond.
The reflective paint formulation of the present invention has several variations depending on the application to include the type of surface to which the paint will be applied. At its most basic formulation, the reflective paint combines the following three ingredients: a single liquid solvent, binder particles, and light scattering particles. For some substrate surface materials, a second liquid solvent can be added to improve adherence of the reflective paint and/or prevent reaction/corrosion between the reflective paint and the underlying substrate surface material. The basic paint formulation using one liquid solvent as well as two additional paint formulations adding a second liquid solvent are presented in the table below.
Paint Formulations
Solvent
Solvent
Solvent A
Solvent B
Binder
Scatterer
A
B
Weight %
Weight %
Weight %
Weight %
Water
N/A
42.4-71.3
N/A
14.4-28.3
14.3-29.3
Water
Methanol
44.1-48.0
14.7-16.0
16.5-18.1
17.9-24.7
Water
Ethanol
45.4-51.7
15.1-17.2
15.2-17.3
13.8-24.2
For each of the three formulations noted in the table, the water solvent is purified water such as what is known as “nanopure water” that is defined as having an ionic purity of at least 18.2 megohms. A variety of commercially-available lab water systems can be used to generate such purified water as is well-known in the art.
The binder materials for each of the three formulations are particles prior to the fabrication process. However, the binder materials must be completely soluble in any of the water, water/methanol, or water/ethanol liquid solvents; remain completely dissolved during paint fabrication as will be described further below; and remain completely dissolved in the final paint's liquid mixture throughout application of the paint to a surface. While the size of the binder particles is not a limitation of the present invention, smaller sizes will hasten their dissolution in water during the paint fabrication process. The binder material must be transmissive or non-absorptive with respect to a significant portion of the radiation within the Sun's spectral emission band. The binder material must also be completely soluble in any of the paint's liquid solvents as noted above. Suitable binder materials include potassium bromide, sodium chloride, potassium chloride, sodium bromide, cesium chloride, and rubidium chloride. Regardless of the choice of binder material, it is preferred that it be at least 99.9% pure.
The scatterer materials for each of the three formulations are particles of light scattering material that are insoluble in any of the paint's liquid solvents and whose particle size generally ranges from 100 to 200 nanometers (nm). The light scattering material must also have a substantially different (and typically greater) index of refraction than the binder material. Suitable light scattering materials include hafnium oxide and yttrium oxide. Regardless of the choice of light scattering material, it is preferred that it be at least 99.9% pure.
For each of the three paint formulations recited in the table above, reflectance performance varies with the weight percent of the ingredients. In general, the various paint mixtures of the present invention will employ approximately the same weight percent of binder particles and light scattering particles. However, it is to be understood that slight variations can be tolerated without affecting paint performance.
Based on empirical and analytic data, a suitable paint formulation for the water-only solvent is approximately 60.8 weight percent water, approximately 19.7 weight percent binder particles, and approximately 19.5 weight percent light scattering particles. For the two-part solvent of water and methanol, a suitable formulation is approximately 48.0 weight percent water, approximately 16.0 weight percent methanol, approximately 18.1 weight percent binder particles, and approximately 17.9 weight percent light scattering particles. For the two-part solvent of water and ethanol, a suitable formulation is approximately 51.7 weight percent water, approximately 17.2 weight percent ethanol, approximately 17.3 weight percent binder particles, and approximately 13.8 weight percent light scattering particles. The formulation using ethanol (as opposed to methanol) reduces the paint's toxicity and is not corrosive to underlying structures made from aluminum alloys and stainless steel.
The process used to fabricate the above described reflective paint formulations will now be described with reference to
Referring first to
Referring next to
The effectiveness of the reflective paint described herein will now be illustrated with reference to
The reflective properties of the present invention's paint will now be explained with reference to
The advantages of the present invention are numerous. The reflective paint greatly increases a structure's reflectance characteristics. The paint nature of the present invention will allow it to be readily used for a variety of structures and systems. The paint formulations are simple and easy to fabricate thereby making them cost-effective solutions in the field of reflective coatings.
Although the invention has been described relative to a specific embodiment thereof, there are numerous variations and modifications that will be readily apparent to those skilled in the art in light of the above teachings. It is therefore to be understood that, within the scope of the appended claims, the invention may be practiced other than as specifically described.
Youngquist, Robert C., Gibson, Tracy L.
Patent | Priority | Assignee | Title |
Executed on | Assignor | Assignee | Conveyance | Frame | Reel | Doc |
Sep 19 2019 | UNITED STATES OF AMERICA AS REPRESENTED BY THE ADMINISTRATOR OF NASA | (assignment on the face of the patent) | / | |||
Sep 20 2019 | YOUNGQUIST, ROBERT C | UNITED STATES OF AMERICA AS REPRESENTED BY THE ADMINISTRATOR OF NASA | ASSIGNMENT OF ASSIGNORS INTEREST SEE DOCUMENT FOR DETAILS | 059804 | /0623 |
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